IP Library Granted Patent US 8,732,920
Granted Patent B2
US 8,732,920 · App. 13/347,108 · Granted May 27, 2014

Tooling and a method for hot forging pieces of sheet metal

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Quick Facts
Patent No.
US 8,732,920
App. No.
13/347,108
Granted
May 27, 2014
Kind
B2
Abstract

The invention provides tooling and a method for hot forging pieces of sheet metal that are to form metal reinforcement mounted on the leading or trailing edge of a turbine engine blade, by means of bottom and top matrices each presenting a twisted elongate surface for use in shaping an initially plane piece of sheet metal, the shaping surface of the bottom matrix presenting a high portion, a low portion, and two end zones. The bottom matrix includes studs for positioning and guiding the piece, the studs being situated at the periphery of the corresponding shaping surface.

Claims (12)

1. A tooling for hot forging pieces of sheet metal that form metal reinforcements mounted on leading or trailing edges of turbine engine blades, the tooling comprising:

a bottom matrix including a first shaping surface that is a twisted elongate surface;

a top matrix including a second shaping surface that is a twisted elongate surface;

wherein the bottom matrix and top matrix are for use in shaping an initially plane piece of sheet metal,

wherein the first shaping surface includes a high portion, a low portion in a position below the high portion in a vertical direction, and two end zones on opposite sides of the first shaping surface,

wherein the bottom matrix includes at least three studs extending above the high portion in the vertical direction for positioning and guiding the initially plane piece of sheet metal, the at least three studs being situated at a periphery of the first shaping surface and including:

a first stud and a second stud positioned at respective end zones of the first shaping surface, and

a third stud extending from a position in the vertical direction below the low portion of the first shaping surface and having a length greater than respective lengths of the first stud and the second stud.

2. Tooling according to claim 1 , wherein the at least three studs are situated on one side of a middle longitudinal axis of the first shaping surface of the bottom matrix.

3. Tooling according to claim 1 , wherein the length of the third stud is not less than a difference between a height of the high portion and a height of the low portion of the first shaping surface.

4. Tooling according to claim 1 , wherein at least one stud of the at least three studs extends perpendicularly to the periphery of the first shaping surface and has a section that tapers towards an inside of the first shaping surface and forms a point or line bearing zone for an edge of the initially plane piece of sheet metal.

5. Tooling according to claim 1 , wherein the bottom matrix includes a fourth stud situated level with the high portion of the first shaping surface in a zone of greatest curvature of a corresponding edge of first the shaping surface.

Assignments (3)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 10, 2012
From: LECONTE, GILBERT MICHEL MARIN; FRANCHET, JEAN-MICHEL PATRICK MAURICE; KLEIN, GILLES CHARLES CASIMIR; MAGNAUDEIX, DOMINIQUE
To: SNECMA
Reel/Frame 027509/0884 →